Torque measurement tester for a hole treating rotary tool

ABSTRACT

Proposed is a torque measurement tester for testing hole-treating rotary tools used on hole treating operations such as drilling, tapping, reaming, countersinking, or the like under real operation conditions for determining the most optimal operations parameters. The torque measurement unit consists of a package of three sensor units, in which the first unit is connected to the frame of the tester via pressure sensors for measuring a thrust force acting in the Z-axis direction, the second sensor unit measures forces acting on the tool in the direction of the X-axis, and the third sensor unit measures forces acting in the Y-axis direction. All measurements are carried out irrespective of each other without mutual effect on the measurement data. The third unit resiliently supports the rotary tool relative to the second unit, while the second unit is connected to the first sensor unit.

BACKGROUND OF THE INVENTION Field of the Invention

The invention relates to a torque measurement tester for rotary tools used on hole treating operations such as drilling, tapping, reaming, countersinking, or the like. More specifically, the invention relates to a torque measurement tester for testing hole treating tools such as drills, tapping tools, countersinking tools, reaming tools, or the like, under real operation conditions for determining the most optimal operation parameters and conditions, such as a thrust force, amount of feed, rotation speed, driving power, friction force, etc.

Description of the Related Art

It is known that during such operations as drilling, tapping, countersinking, reaming, or the like, the optimal work of a rotary tool depends on many factors such as a thrust force, geometry of the tool, drive torque, friction conditions on the treated surface, amount of feed, etc.

Some devices known heretofore for testing rotary tools on hole treating operations are based on measuring a torque developed during the operation.

For example, U.S. Pat. No. 4,583,411 describes a method and apparatus for dynamically testing a rotational torque-producing device during calibration under conditions simulating actual operating conditions. The torque produced by the torque-producing device under controlled load conditions similar to actual operating conditions is converted by a transducer to an electrical signal and monitored to assure that the stall torque is maintained within an acceptable band.

U.S. Pat. No. 2,791,304 describes a tapping tool equipped with a device for stopping the turning action on the tool when the strain reaches a predetermined or excessive amount and fully releasing the torque or twist on the tap until the tap is withdrawn. The device also includes protective means for preventing breakage of the taps under various unusual conditions.

Chinese Patent Application Publication No. 1,394,712 describes a method and apparatus for on-line fault diagnosis of vibration threading. The apparatus includes a vibration threading machine unit, a drive, a control unit of the stepper motor, a torque measuring unit, a torque sensor, and a threading torque analysis and storage system, which are series-connected between the main shaft input end and a threading grip holder. The torque sensor is fixedly connected with the main shaft of the threading machine by means of an elastic holding mechanism formed from an elastic holder base cover, a locking cover, and locking screw.

U.S. Pat. No. 8,556,000 discloses a device for monitoring a drilling or coring operation and an installation comprising such a device. The device comprises equipment for measuring parameters of a drilling or coring operation by means of a drill bit fixed to the end of a drill string, measurement equipment being housed in a chamber made in a coupling that is designed to be interposed between two drill string pipes or between the drill bit and a drill string pipe, or to constitute an adapter for a cutting head of the drill bit of a drill string.

U.S. Pat. No. 4,649,757 discloses a device for calibrating a machine tool including a cutting tool rotating about its axis and comprising a tubular-shaped support with an annular fixing component connecting the support to the housing of the machine tool so that its central opening forms an extension of the opening of the housing for the passage of the tool. The support also has at least one part which is deformable under the action of twisting about the aforementioned axis and is provided with at least one strain gauge and an end part which is opposite the fixing component and in which there is arranged, along the axis of the support, a component for connecting the end of the tool, which component is provided with means enabling locking of said tool in rotation with the connection component. The latter carries a disk located between two annular components held against the disk by adjustable means. As a result of a measuring means associated with the strain gauge, a current representing the resisting torque opposing the tool may be measured via the disk and other components. The invention relates, in particular, to machines for screwing the partitioning of a nuclear reactor core.

SUMMARY OF THE INVENTION

The invention relates to a torque measurement tester for rotary tools used on hole treating operations (hereinafter referred to as a “tester” or a “tester of the invention”) such as drilling, tapping, reaming, countersinking, or the like. More specifically, the invention relates to a torque measurement tester for testing the hole treating tools such as drills, tapping tools, countersinking tools, reaming tools, or the like under real operation conditions for determining the most optimal operation parameters and conditions, such as a thrust force, amount of feed, rotation speed, driving power, friction force, etc.

It is known that during such operations as drilling, tapping, countersinking, reaming, or the like, the optimal work of a rotary tool depends on many factors such as a thrust force, geometry of the tool, drive torque, friction conditions on the treated surface, amount of feed, deviation of the rotary tool from the axis of rotation, etc.

In view of the above, the invention provides a tester for testing a hole treating tool under conditions similar to the use of the tool under real production conditions. The tester allows independent measurement of a force applied to the tool during a hole treatment operation in the axial direction of the tool and forces acting on the tool in two mutually perpendicular directions, which are also perpendicular to the axial direction of the rotary tool. The first direction is a Z-axis direction, the second direction is a X-axis direction, and the third direction is a Y-axis direction in an orthogonal X-Y-Z coordinate system. The independent measurement of all three forces without mutual influence on each other is possible by making the torque measurement unit of the tester in the form of a three-layered structure consisting of a first sensor unit with first sensors measuring a thrust force acting in the Z-axis direction, a second sensor unit with second sensors for measuring a pair of forces acting in the X-axis direction, and a third sensor unit for measuring a pair of forces acting in the Y-axis direction, and a tool holding unit which resiliently supports the tool to be used on the hole treatment operation. The first sensor unit is attached to the frame of the sensor through the first sensors which constitute pressure sensors measuring a thrust force applied to the tool. The third sensor unit is a unit of a package composed of two identical flexible parallelograms, which are turned by 90° to each other around the axial direction, i.e., the axis of rotation of the tool, wherein each parallelogram consists of an upper sensor-holding plate and a lower-sensor holding plate. Both plates are interconnected via flexible beams, which allow coplanar movements of the upper sensor-holding plate and the lower-sensor holding plate relative to each other. Since the parallelograms are turned by 90° to each other around the axial direction of the rotary tool, the beams allow flexible movements of the respective plates in the X-axis and Y-axis directions. The upper sensor holding plate of the upper parallelogram of the third sensor unit is rigidly attached to the first sensor unit, while the lower sensor-holding plate of the lower parallelogram of the third sensor unit is connected to the tool holding unit.

The package does not limit independent movements of the at least two second sensors and at least two third sensors, the resilient tool holder being resiliently connected to the second sensor unit via the springing device.

Thus, it becomes possible to independently measure the forces acting in all three directions without a mutual influence onto the measurement results, to calculate torques developed on the tool, and find the conditions most optimal for reproduction of the results of measurements and calculations on the production equipment during manufacturing under industrial conditions.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are incorporated in and constitute a part of this specification exemplify the embodiments of the present invention and, together with the description, serve to explain and illustrate principles of the inventive technique. Specifically:

FIG. 1A is a general side view of the torque measurement tester of the invention for testing a hole treating rotary tool.

FIG. 1B is an exploded side view of the torque measurement unit of the tester of FIG. 1A.

FIG. 2 is an exploded perspective view of a force measurement unit used in the torque measurement unit of the tester of FIG. 1A.

FIG. 3A is a scheme illustrating forces acting on a rotary tool in the tester of the invention.

FIG. 3B is another view illustrating forces acting on a rotary tool in the tester of the invention.

FIG. 4 is a perspective view of a resilient tool holder used in the torque measurement unit of the tester of the invention.

FIG. 5A is a top view illustrating the angular deviation of the first force measurement unit under effect of a pair of forces acting in the X-axis direction.

FIG. 5B is a top view illustrating the angular deviation of the first force measurement unit under effect of a pair of forces acting in the Y-axis direction.

FIG. 6A is a diagram illustrating directions of forces that cause deformations shown in FIG. 5A.

FIG. 6B is a diagram illustrating directions of forces that cause deformations shown in FIG. 5B.

FIG. 7A is a side view of the resilient tool holder unit of FIG. 4 under no-load conditions.

FIG. 7B is a side view of the resilient tool holder unit of FIG. 4 illustrating deformations of the holder unit in the Z-axis direction under the effect of a vertical load applied to the tool from the test specimen.

DETAILED DESCRIPTION

In the following detailed description, reference will be made to the accompanying drawing(s), in which identical functional elements are designated with like numerals. The aforementioned accompanying drawings show by way of illustration, and not by way of limitation, specific embodiments and implementations consistent with principles of the present invention. These implementations are described in sufficient detail to enable those skilled in the art to practice the invention and it is to be understood that other implementations may be utilized and that structural changes and/or substitutions of various elements may be made without departing from the scope and spirit of present invention. The following detailed description is, therefore, not to be construed in a limited sense.

The invention relates to a torque measurement tester for rotary tools used on hole treating operations (hereinafter referred to as a “tester” or a “tester of the invention”) such as drilling, tapping, reaming, countersinking, or the like. More specifically, the invention relates to a torque measurement tester for testing the hole treating tools such as drills, tapping tools, countersinking tools, reaming tools, or the like under real operation conditions for determining the most optimal operations parameters and conditions, such as a thrust force, amount of feed, rotation speed, driving power, friction force, etc.

It is known that during such operations as drilling, tapping, countersinking, reaming, or the like, the optimal work of a rotary tool depends on many factors such as a thrust force, geometry of the tool, drive torque, friction conditions on the treated surface, amount of feed, etc.

In view of the above, the invention provides a tester for testing a hole treating tool under conditions similar to the use of the tool under real production conditions. The tester allows independent measurement of a force applied to the tool during the hole treatment operation in the axial direction of the tool and forces acting on the tool in two mutually perpendicular directions, which are also perpendicular to the axial direction of the rotary tool. The first direction is a Z-axis direction, which coincides with the longitudinal axis O-O of the rotary head and, hence, of the rotary tool, the second direction is a X-axis direction, and the third direction is a Y-axis direction in an orthogonal X-Y-Z coordinate system. The independent measurement of all three forces without mutual influence on each other is possible by making the torque measurement unit of the tester in the form of a three-layered structure consisting of a first sensor unit with first sensors measuring a thrust force acting in the Z-axis direction, a second sensor unit with second sensors for measuring a pair of forces acting in the X-axis direction, and a third sensor unit for measuring a pair of forces acting in the Y-axis direction, and a tool holding unit which resiliently support the tool to be used on the hole treatment operation. The first sensor unit is attached to the frame of the sensor through the first sensors which constitute pressure sensors measuring a thrust force applied to the tool. The second sensor unit and a third sensor unit form a package composed of two identical flexible parallelograms, which are turned by 90° to each other around the axial direction of the rotary tool, i.e., the axis of the tool rotation, wherein each parallelogram consists of an upper sensor-holding plate and a lower-sensor holding plate. Both plates are interconnected via flexible beams, which allow coplanar movements of the upper sensor-holding plate and the lower-sensor holding plate relative to each other. Since the parallelograms are turned by 90° to each other, the beams allow flexible movements of the respective plates in the X-axis and Y-axis directions. The upper sensor-holding plate of the upper parallelogram of the third sensor unit is rigidly attached to the first sensor unit, while the lower sensor-holding plate of the lower parallelogram of the third sensor unit is connected to the tool holding unit.

Thus, it becomes possible to independently measure the forces acting in all three directions without mutual affect onto the measurement results, calculate torques developed on the tool, and find the conditions most optimal for reproduction of the results of measurements and calculations on the production equipment during manufacturing under industrial conditions.

FIG. 1A is a general side view of the torque measurement tester, which in its entity is designated by reference numeral 20. The tester 20 contains a rigid frame 22 that supports a sample support unit 24 at the lower side, a thrust developing unit 26 at the upper side, and a torque measurement unit 28 having a rotary head 32 which holds a rotary tool 38 that is resiliently attached to the resilient tool holder 31 via a springing device 30. The rotary head and, hence, the rotary tool, have a longitudinal axis O-O (FIG. 1B).

The rotary head 32 has a rotary drive motor 34 and a tool holder 36 that is intended for securing the rotary tool 38, e.g., a tapping tool, which is to be tested.

The thrust developing unit 26, which applies a force to the torque measurement unit, and hence to the rotary tool 38, can move in the direction of the arrows Z and is guided in this direction in the guides 39 of a carriage 40. The carriage 40, in turn, can be driven in the direction of arrow X perpendicular to the Z-direction along guides 42 installed on the frame 22.

Reference numeral 44 designates a schematically shown combined driver unit for controlling drives in the, X, Y, and Z directions, where Y-axis is perpendicular to the plane of the drawing in side view of FIG. 1A. Reference 46 designates a CPU which collects all data obtained from the sensors (described below) and controls the operation of the tester through the computer 47. The reference numeral 48 designates an acoustic sensor, and 49 designates a tool cleaning station. The devices 44, 46, 47, 48, and 49 are subjects of other patent applications and are beyond the scope of the present invention.

Having described the torque measurement tester 20 in general, let us consider the main components of the tester 20 in detail separately.

The structure of the torque measurement unit 28 is shown in more detail in FIG. 1B, which is an exploded side view of the torque measurement unit 28 of the tester of FIG. 1A.

In FIG. 1B, reference numeral 41 designates a thrust force measurement unit which contains pressure sensitive members 80 a and 80 b that are deformed under the effect of a compression force and that support respective pressure sensors 80 a-1, 80 b-1. There may be two other similar sensors which cannot be seen in the drawing. The pressure sensors 80 a-1, 80 b-1 are force sensors, e.g., of a strain-gauge type. The pressure sensitive members, which are deformed under the effect of a compression force of the thrust developing unit 26 are sandwiched between an upper thrust unit plate 82, which is rigidly connected to the thrust developing unit 26, and a lower thrust unit plate 84, which is rigidly connected to a third force measurement sensor unit 52, which is described below.

More specifically, in addition to the thrust force measurement unit 41, the sensor 20 of the invention is provided with a sensor unit package 53 (FIG. 1B) composed of a second sensor unit 50 with second sensors and a third sensor unit 52, which is similar to the sensor unit 50 but is turned by 90° relative to the second sensor unit 50. The sensor units 50 and 52 are interconnected through a gasket 54.

Since the second and third sensor units are identical, let us consider in detail only one of them, e.g., the third sensor unit 52, which is shown in FIG. 2 in the form of an exploded view.

As can be seen from FIG. 2, each sensor unit 50 or 52 consists of an upper sensor-holding plate 52 a and a lower sensor-holding plate 52 b. Each sensor-holding plate has rigid blocks at two diametrically opposite corners firmly attached to the respective sensor-holding plates. Thus, the upper sensor-holding plate 52 a has a rigid block 52 a 1 (shown by broken lines in FIG. 2) and a diametrically opposite rigid block 52 a 2. On the other hand, the lower sensor-holding plate 52 b has a rigid block 52 b 1 and a diametrically opposite rigid block 52 b 2. Attached to the inward facing surface of the block 52 a 1 is a flexible beam 58 c 1 that in the illustrated embodiment extends parallel to the side 52 a′ of the plate 52 a, i.e., to the axis X (see FIG. 1). Similarly, attached to the inward facing surface of the block 52 b 1 is a flexible beam 52 c 2 that in the illustrated embodiment extends parallel to the side 52 b′ of the plate 52 b, i.e., to the axis Y (see FIG. 1A).

In an assembled state of the force sensor measurement unit 50 shown in FIG. 2, the flexible beam 52 c 1 is spaced from the surface of the upper sensor-holding plate 52 a with the gap G1 (FIG. 1B), and flexible beam 52 c 2 is spaced from the surface of the lower sensor-holding plate 52 a with the gap G2, which is equal to the gap G1. In fact, both flexible beams are spaced from both upper and lower plates so that the plates and beam together form a flexible parallelogram with the upper plate 58 a and the lower plate 58 b flexibly moveable coplanar to each other when the flexible beams 58 c 1 and 58 c 2 are resiliently deformed.

In other words, the rigid blocks 52 a 1, 52 a 2, 52 b 1, and 52 b 2 function as spacers that space the upper sensor-holding plate 58 a and the lower sensor-holding plate 58 b parallel to each other and at a certain distance from each other, while the flexible beams 58 c 1 and 58 c 2 function like resilient members that allow the plates to shift coplanar to each other in the horizontal direction under the effect of a friction force Ff acting, e.g., in the direction perpendicular to the X-axis direction (see FIGS. 3A and 3B), that may occur between the outer side surface of the hole treating tool 38 and the inner wall 60 of the hole 62 treated by the tool 38 in a sample S (FIG. 3A) installed in the sample holder 24 (FIG. 1).

Thus, each of the sensor blocks 50 and 52 is made in the form of a package of two identical flexible parallelograms, which are turned by 90° to each other around the axial direction, wherein each parallelogram consists of an upper sensor-holding plate, such as the plate 52 a, and a lower-sensor holding plate, such as the plate 52 b, where both plates are interconnected via flexible beams 52 c 1 and 52 c 2. The flexible beams allow coplanar movements of the upper sensor-holding plate 52 a and the lower-sensor holding plate 52 b relative to each other. Since the parallelograms are turned by 90° to each other around the axial direction of the tool, the beams allow independent flexible movements of the respective plates in the X-axis and Y-axis directions.

In other words, the package 53 does not limit independent movements of the at least two second sensors of the sensor unit 50 and the at least two third sensors of the sensor unit 52. It is also seen from FIG. 4 that the resilient tool holder 31 is resiliently connected to the second sensor unit 50 via the springing device 30.

FIG. 3A is a scheme illustrating forces acting on a rotary tool in the tester of the invention. A local change of the friction force Ff may be caused by such factors as wear of the tool cutting edges, contamination of the treated hole 62 with cutting debris, lack of proper lubrication, etc. In FIG. 3A, R designates a tool radius, Fn is a vertical thrust force, w is an angular rotation speed developed by the rotary drive motor 34 (FIG. 1), and Ft is a cutting force applied to the treated material from the cutting edges of the tool 38. It is assumed that in a first approximation the friction force Ff is a reaction to the force Ft. In FIG. 3A the arrowed circle shows direction of rotation of the rotary tool 38.

If during a hole treating operation such as tapping, drilling, countersinking, etc., the angular rotation speed w remains constant, the aforementioned forces Ff and Ft are in balance. However, any local changes in the force Ft caused by the aforementioned factors will cause changes in the force Ff. The cutting force torque Tc developed during cutting on the rotary cutting tool 38 is defined as a vector product of the cutting force, i.e., the product of Ft force on the tool radius R. Similarly, the product of the Ff on the tool radius R is defined as a resistance torque Tr. As a result, the change in the forces or imbalance in the values of the torques Tc and Tr leads to changes in the treatment conditions. It is understood that normal cutting conditions will be provided when the torques Tc and Tr are in balance, and measurement under such torque balance conditions will allow to determine such process parameters as speed of rotation, thrust force, tool feed, tool geometry, lubricant etc., which will provide reliable hole treatment operation when the treatment conditions selected on the tester 20 will be observed on the real production equipment.

FIG. 3B is another view illustrating forces acting on a rotary tool in the tester of the invention. This drawing illustrates, e.g., a tapping operation where the tool 38 is a tapping tool that cuts a thread in the hole of the material sample S secured in the sample holder 24. This drawing shows two pairs of forces F1 x-F2 x acting in the directions perpendicular to the X-axis and F1 y-F2 y acting in the directions perpendicular to the Y-axis. As mentioned above, the treatment conditions at which the pairs of forces F1 x-F2 x and F1 y-F2 y are in balance are the goal of the tests conducted on the tester 20.

FIG. 4 is a three-dimensional view of the resilient tool holder unit 31, which constitutes an important part of the torque measurement unit 28.

The resilient probe holder unit 31 consists of a probe-holder upper plate 64 and a probe-holder lower plate 66 having dimensions smaller than the probe-holder upper plate 64. The probe-holder upper plate 64 and the probe-holder lower plate 66 are spaced from each other in a vertical direction by inner spacers 68 a and 68 b.

Attached to the ends of the probe-holder upper plate 64 are outer spacers 70 a and 70 b that are located outward from the inner spacers 68 a and 68 b and hang downward from the probe-holder upper plate 64 so that they are horizontally aligned with the inner spacers 68 a and 68 b.

The inner and upper spacers 68 a and 68 b and 70 a and 70 b, respectively, are interconnected via the springing device 31 that consists of a set of leaf springs 72 a, 72 b, 74 a, 74 b, etc. (the springs located on the other sides of the plates are not seen in the drawings; in this embodiment, the total number of springs is eight). In such a construction, the probe-holder upper plate 64 is rigidly attached to the lower sensor-holding plate 52 b of the second sensor unit 52 (FIG. 2), while the probe-holder lower plate 66 that rigidly holds the rotary tool 38 is resiliently attached relative to the probe-holder upper plate 64 and may perform resilient vertical movements in the direction of the Z-axis together with the rotary head tool 38 attached to this plate. In other words, the tool holder 36, and hence, the rotary head 32, are attached to the probe-holder lower plate 66 of the springing device 30 and is resiliently connected to the probe-holder upper plate 64 via the set of the leaf springs 72 a, 72 b, 74 a, 74 b, etc.

Thus, it is understood that in the torque measurement unit 28 of the tester 20 of the present invention the upper and lower plates 52 a and 52 b contained in the third force measurement sensor unit 52 have freedom of movements only in the Y-axis direction and are restrained from the movements in the X-axis direction. On the other hand, the upper and lower plates (not shown, as the structures of the units 50 and 52 are identical), contained in the second force measurement sensor unit 50 have freedom of movements only in the X-axis direction and are restrained from the movements in the Y-axis direction. As a result, it is obvious that each force sensor measurement unit that contains two force measurement sensors, preferably of strain-gauge type, such as the sensors 52 c 1-1 and 52 c 2-1 (FIG. 2), allows to measure the pair of forces which twists one of the force measurement sensor unit. Such a condition is shown in FIG. 5A, where the first force measurement sensor unit 50 is shown in a deformed and twisted position relative to the second force measurement sensor unit 52 under the effect of the pair of forces acting in the direction of the X-axis. Similarly, FIG. 5B shows the second force measurement sensor unit 52 in a deformed and twisted position relative to the first force measurement sensor unit 50 under the effect of the pair of forces acting in the direction of the Y-axis.

FIG. 6A is a diagram illustrating directions of forces that cause deformations shown in FIG. 5A.

FIG. 6B is a diagram illustrating directions of forces that cause deformations shown in FIG. 5B.

These diagrams show angular deformations of the force measurement sensor units in the X-Y plane. For better understanding the principle of deformations of the units the twist angles α and α′, as well as the deformed shapes depicted by broken lines are shown in an exaggerated form. Since in reality the twist angles α and α′ are extremely small, the angular deformations may be neglected. Thus it can be assumed that the torques are produced by pairs or forces measured in two mutually perpendicular directions.

FIG. 7A is a side view of the resilient tool holder unit of FIG. 4 under no-load conditions.

FIG. 7B is a side view of the resilient tool holder unit of FIG. 4 illustrating deformations of the holder unit in the Z-axis direction under the effect of a vertical load applied to the tool from the test specimen. It can be seen from FIG. 7B that when during a treatment operation the rotary tool 38 experiences resistance to the vertical thrust force Fv applied from the thrust developing unit 26, this causes deformation of the leaf springs such as the leaf springs 72 a, 72 b, 74 a, and 74 b which is shown in FIG. 7B. In this case, through the springing package 30 the force of the leaf springs 72 a, 72 b, 74 a, and 74 b is transmitted to the thrust force measurement unit 41 and, in fact, to the pressure sensors, such as sensors 80 a-1, 80 b-1 (FIG. 1B). The measurement of the thrust force F and, in fact, of the resistance to the feed of the rotary tool in the vertical direction toward the sample S is carried out independently from measurements of the torque. In other words, the measurement of the forces acting in the X-Y plane and in the Z-axis direction do not affect each other, i.e., can be performed without mutual cross-talks.

The pressure sensors can be represented by tension sensors, film piezo sensors, or the like and can be pasted to the deformable surfaces in a manner known in the art. The number and arrangement of the sensors may vary but for convenience of operation and calibration it is recommended that the sensors on the pressure sensitive members, such as the sensors 80 a-1 and 80 b-1, be arranged opposite to each other in the diagonal direction. In fact, there are four such sensors in opposite corners of the upper thrust unit plate 82 but only two of them are shown.

In operation, a rotary tool 38, which constitutes an object of the test, is tested on various specific operations for which it is intended to be used under real manufacturing conditions, e.g., in mass production on production equipment. The test operations are carried out by using different materials, instruments with different geometries, different lubricant, tool feeds, thrust forces, etc. The forces acting on the tool during the test, i.e., the vertical thrust force FV (FIG. 1A), and two mutually perpendicular horizontal forces, such as F1 x, F2 x and F1 y, F2 y (FIG. 3B), are measured simultaneously and independently from each other. Since the data obtained in the test will be then used in a real production process, it is extremely important to carry out the tests under conditions of high accuracy and reproducibility of the obtained results. This is achieved due to independence in measurement of forces acting on the tool from different directions.

If the rotary tool 38 operates under normally selected conditions and operation parameters, there will be no misbalance between the data obtained from the X and Y-axes sensors, such as sensors 52 c 1-1, 52 c 1-1, etc. When during the test of the rotary tool the torque is abnormally grows, e.g., because of the increased friction between the rotary tool and the inner walls of the hole being treated, to the extent that leads to distortion or deflection of the tool axis relative to the axis of the treated hole, this phenomenon will cause difference in signals obtained on X and Y-axes sensors. For example, such an effect may be observed if the direction of the vertical force FV applied to the tool has been deviated from the axis of tool rotation. A similar effect may occur in treating holes formed in composite material made from components having different densities, or the like.

Although the torque measurement tester 20 of the invention has been described with reference to specific examples shown in specific drawings, it is understood that any changes or modification are possible without deviation from the scope of the attached claims. For example, the tool may be exemplified not only by drills, tapping tools, countersinking tools, but also by rotating material specimens, or the like. The tester may be provided with an acoustic sensor for acoustically sensing abnormalities that may occur during the test, e.g., when the hole in the sample material is clogged with cutting debris. 

What is claimed is:
 1. A torque measurement tester for a hole treating rotary tool comprising: a frame; a sample support unit and a thrust developing unit that are attached to the frame; a torque measurement unit that comprises: a rotary head that comprises a rotary drive motor, a resilient tool holder, and a rotary tool having a longitudinal axis and held by the resilient tool holder; a first sensor unit with at least one first sensor for measuring forces applied to the rotary tool in the direction of the longitudinal axis of the rotary tool; a resilient tool holder unit having a springing device for resiliently supporting the rotary head; a second sensor unit with at least two second sensors for measuring forces applied to the rotary tool in a second direction; and a third sensor unit with at least two third sensors for measuring forces applied to the rotary tool in a third direction, respectively, wherein the second and the third directions are perpendicular to the longitudinal axis of the rotary tool and to each other and wherein the first sensor unit is connected to the frame via the at least one first sensor, while the second sensor unit and the third sensor unit are integrally connected into package without limitation of independent movement of the at least two second sensors and at least two third sensors, the resilient tool holder being resiliently connected to the second sensor unit via said springing device.
 2. The torque measurement tester according to claim 1, wherein the second sensor unit and the third sensor unit in said package are identical but arranged relative to each other with their respective at least two second sensors and at least two third sensors turned by 90° around the axial direction.
 3. The torque measurement tester of claim 2, wherein the at least one first sensor, the at least two second sensors and the at least two third sensors are force measurement sensors.
 4. The torque measurement tester according to claim 3, wherein the second sensor unit and the third sensor unit are identical and each comprises a parallelogram comprising an upper plate, a lower plate, and flexible beams interconnecting the upper plate with the lower plates, the second sensors being installed on the flexible beams of the second sensor unit, and the third sensors being installed on the flexible beams of the of the third sensor unit.
 5. The torque measurement tester according to claim 4, wherein the upper plate or lower plate of one of the parallelograms is flexibly moveable in said second direction independently of the upper plate or lower plate of the other of the parallelograms which is flexibly moveable in said third direction.
 6. The torque measurement tester of claim 1, wherein the resilient tool holder comprises a probe-holder upper plate and a probe-holder lower plate, which are spaced from each other in the direction of the longitudinal axis of the rotary tool and which are interconnected through the springing device, wherein the probe-holder upper plate is connected to the lower plate of the second sensor unit, and the probe holder lower plate supports the rotary head.
 7. The torque measurement tester according to claim 6, wherein the second sensor unit and the third sensor unit in said package are identical but arranged relative to each other with their respective at least two second sensors and at least two third sensors turned by 90°.
 8. The torque measurement tester of claim 7, wherein the at least one first sensor, the at least two second sensors and the at least two third sensors are force measurement sensors.
 9. The torque measurement tester according to claim 8, wherein the second sensor unit and the third sensor unit are identical and each comprises a parallelogram comprising an upper plate, a lower plate, and flexible beams interconnecting the upper plate with the lower plates, the second sensors being installed on the flexible beams of the second sensor unit, and the third sensors being installed on the flexible beams of the of the third sensor unit.
 10. The torque measurement tester according to claim 9, wherein the upper plate or lower plate of one of the parallelograms is flexibly moveable in said second direction independently of the upper plate or lower plate of the other of the parallelograms which is flexibly moveable in said third direction.
 11. The torque measurement tester according to claim 1, wherein the springing device comprises a tool-holder upper plate which is connected to the lower plate of the second sensor unit, a tool-holder lower plate that supports the tool holder of the rotary tool, and a set of springs that connects the tool-holder lower plate to the tool-holder upper plate.
 12. The torque measurement tester according to claim 11, wherein the second sensor unit and the third sensor unit in said common sensor unit are identical but arranged relative to each other with their respective at least two second sensors and at least two third sensors turned by 90°.
 13. The torque measurement tester of claim 12, wherein the at least one first sensor, the at least two second sensors and the at least two third sensors are force measurement sensors.
 14. The torque measurement tester according to claim 13, wherein the second sensor unit and the third sensor unit are identical and each comprises a parallelogram comprising an upper plate, a lower plate, and flexible beams interconnecting the upper plate with the lower plates, the second sensors being installed on the flexible beams of the second sensor unit, and the third sensors being installed on the flexible beams of the of the third sensor unit.
 15. The torque measurement tester according to claim 14, wherein the upper plate or lower plate of one of the parallelograms is flexibly moveable in said second direction independently of the upper plate or lower plate of the other of the parallelograms, which is flexibly moveable in said third direction.
 16. The torque measurement tester according to claim 1, wherein the rotary tool is selected from the group consisting of drills, tapping tools, countersinking tools, and reaming tools.
 17. The torque measurement tester according to claim 1, wherein the rotary tool is selected from the group consisting of drills, tapping tools, countersinking tools, and reaming tools.
 18. The torque measurement tester according to claim 5, wherein the rotary tool is selected from the group consisting of drills, tapping tools, countersinking tools, and reaming tools.
 19. The torque measurement tester according to claim 9, wherein the rotary tool is selected from the group consisting of drills, tapping tools, countersinking tools, and reaming tools.
 20. The torque measurement tester according to claim 14, wherein the rotary tool is selected from the group consisting of drills, tapping tools, countersinking tools, and reaming tools. 